| タイトル | Dynamics and identification of flexible aircraft |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760014070 |
| 著者（英） | Wells, W. R. |
| 著者所属（英） | Cincinnati Univ. |
| 発行日 | 1976-04-01 |
| 言語 | eng |
| 内容記述 | The equations of motion and a maximum likelihood parameter identification formulation are developed for a flexible aircraft. The various levels of approximation associated with the modal substitution representation of the elastic displacement field are discussed and illustrated when appropriate. The necessary extension of the parameter set of stability and control derivatives due to the aeroelastic effects is obtained. |
| NASA分類 | AERODYNAMICS |
| レポートNO | 76N21158
NASA-CR-2672 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186432 |
